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Results: 1 through 12 of 12 (0.211 secs)
You searched for: (collection:ufnaca OR mediatype:ufnaca) AND -mediatype:collection AND firstTitle:D
[texts]Determination of desirable lengths of Z- and channel-section columns for local-instability tests - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806705&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Design and construction; Aerodynamics--Research
Downloads: 86
[texts]Determination of effective column length from strain measurements - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804669&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes, Tailless; Aerodynamics--Research
Downloads: 88
[texts]Determination of induced velocity in front of an inclined propeller by a magnetic-analogy method - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003596963&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aeronautics--Research
Downloads: 120
[texts]Determination of jet-boundary corrections to cowling-flap-outlet pressures by an electrical analogy method - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805105&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Motors--Cowlings; Airplanes--Nacelles; Aerodynamics--Research
Downloads: 87
[texts]Determination of the effect of horizontal-tail flexibility on longitudinal control characteristics - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003616150&ix=nu&I=0&V=D&pm=1
Keywords: Fighter planes; Aerodynamics--Research
Downloads: 102
[texts]Determination of the stability and control characteristics of a straight-wing, tailless fighter-airplane model in the Langley free-flight tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804669&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes, Tailless; Aerodynamics--Research
Downloads: 73
[texts]Determination of the stability and control characteristics of a tailless all-wing airplane model with sweepback in the Langley free-flight tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003616137&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes, Tailless; Aerodynamics--Research
Downloads: 85
[texts]Determination of the stress concentration factor of a stepped shaft stressed in torsion by means of precision strain gages - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003760230&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Torsion; Strains and stresses--Research
Downloads: 212
[texts]Development of a laminar boundary layer behind a suction point - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779451&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar boundary layer
Downloads: 74
[texts]Development of cowling for long-nose air-cooled engine in the NACA full-scale wind tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805104&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Motors--Cowlings; Aerodynamics--Research
Downloads: 84
[texts]Displacement effect of the laminar boundary layer and the pressure drag - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779843&ix=nu&I=0&V=D&pm=1
Keywords: Drag (Aerodynamics; Laminar boundary layer
Downloads: 162
[texts]Drag reduction by suction of the boundary layer separated behind shock wave formation at high mach numbers - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003760239&ix=nu&I=0&V=D&pm=1
Keywords: Drag (Aerodynamics; Boundary layer
Downloads: 87
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